Research Work
at
International Center for Nano Technology
and Applied Adhesion
Proposal full title: High Performance Nano Adhesive Bonding of Space Durable Polymer and its Stability at Geosynchronous Earth Orbit
Principal Investigators:
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Prof. Dr. Sangeeta Jha,
Department of Chemistry, Sikkim Manipal Institute of
Technology |
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Prof. Dr. Sushabhan
Choudhury, Department of Electronics and
Communication Engineering, |
Co-Investigators (International
Collaborators):
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Dr. J. A. Poulis,
Director, Adhesion Institute, Faculty of Aerospace
Engineering, Delft University of Technology, |
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Dr. Shantanu Bhowmik,
Senior Scientist, Faculty of Aerospace |
Objective:
Work of particular relevance to this proposal has been on
the enhancement of adhesion and of bond durability of high
temperature resistant polymer such as Polyimide, which can
follow surface treatments through low-pressure plasma, which
increases wetting characteristics of the substrate surface,
followed by preparation of high performance nano adhesive by
dispersing Carbon Nano Fiber (CNF) in ultra high temperature
resistant adhesive such as Polyimide adhesive with further
modification of Polyimide Nano Adhesive Bonding under
Electron Beam Irradiation. The work has been designed not
only to improve adhesion characteristics but also keeping in
view of its application to Geosynchronous Earth Orbit (GEO).
Therefore, challenges will be taken for retention of
adhesion and durability of high performance nano adhesive
bonding of space durable polymer when subject to space
climate, especially under high temperature, cryogenic
atmosphere, high energy radiation (gamma rays, proton and
neutron radiation) atmosphere and humid as well as chemical
and other relevant cosmic atmospheres.
Task of the Project:
In search of long time and efficient service performance in
the context of future generation of space applications
especially at GEO, work of particular relevance to this
project has been on the improvement of high performance
polymer-polymer composite through high performance nano
adhesive bonding by exposing the composite under electron
beam irradiation.
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Formation of
ICNTAA Advisory
Committee About
ICNTAA Faculty Members Objectives Collaborating
Partners
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Based on these considerations, high temperature resistant
space durable polymeric sheet such as Polyimide sheet, which
also have excellent cryogenic properties and which can be
joined with Polyimide sheet by employing ultra high
temperature resistant Polyimide adhesive, with dispersing
Carbon Nano Fiber (CNF) into the matrix adhesive as CNF’s
are one of the strongest materials. It is expected that with
the inclusion of CNF in the Polyimide adhesive, the cohesive
strength, toughness and thermal properties of the adhesive
will increase significantly. This is because, local
stiffening due to nano fibers results in much improved load
transfer at the adhesive-CNF interface. Therefore, these
bonding could be highly useful in the structural fabrication
in the space industry. However, these polymers in general
exhibit insufficient adhesive bond strength due to their
reasonably low surface energy. Thus, it is necessary to
modify the surface of the polymer and surface modification
essentially incorporates various polar functional groups on
the polymer surface, which will help to enhance its surface
energy and to improve adhesive bond strength.
Several surface modification methods are employed to modify
the polymer surface, such as chemical treatments, thermal
treatment, mechanical treatment, electrical treatments under
(a) atmospheric pressure plasma (corona discharge), and, (b)
low pressure plasma (glow discharge) and electron beam
radiation treatment. Glow discharge under low-pressure
plasma is a popular technique, which results in better
uniformity in surface modification of the polymers (Yao et
al, 1993; Liston et al, 1993, Akovali et al 1995, Bhowmik et
al 1998, Dutta et al, 1995, Banik et al 1999, Bonin and Bui
2000). Moreover, it is a dry treatment method, which is
better suited for industrial applications. It is now well
established that the glow discharge treatment as well as
electron beam radiation treatment creates physical and
chemical changes such as crosslinking, formation of free
radicals and oxygen functionalisation in the form of polar
groups on polymer surface resulting in improvement of
wetting and adhesion characteristics (Bag et al, 1999;
Liston et al, 1993; Suzuki et al, 1986, Dorn et al 1990,
Alexander et al 1997, Bhowmik et al 2001, Chattopadhyay et
al 2001, Kettle et al 1997, Bonin et al 1998). Further, it
is emphasised that in a glow discharge treatment different
desired gases could be used for generating different gas
plasmas and temperature of gas generally remains low.
Therefore, the plasma plays a predominant role in the
surface modification of polymers.
However, the most important problem in this polymer-polymer
adhesive joint is, this joint will have to encounter space
environments as stated earlier. Therefore, not only the
adhesion in terms of bond strength but also the durability
of the joint at GEO is the major concern. It has been
established that different environments very often attack
particularly to the polymer-adhesive interface. Moreover,
high energy radiation especially gamma radiation is
significantly harmful for polymeric materials and therefore,
premature failure could takes place at the Polymer-adhesive
interface resulting in significantly low joint strength.
In this regard, surface of high performance polymer such as
Polyimide will be modified by using low-pressure plasma at
various process parameters and under various desired process
gases. The surface of carbon nano fibers will be modified by
low-pressure plasma using nitrogen as process gas. This
modification will essentially incorporate polar functional
groups such as carboxyl, carbonyl etc. on the surface of
carbon nano fibers, which would certainly permit better
adhesion with the ultra high temperature resistant polyimide
adhesive. Once the bonding with Polyimide is set and cured,
the entire composite will be modified under electron beam
irradiation, resulting in significant incorporation of
crosslinking within the composite leading to substantial
improvement of mechanical strength.
In view of the above facts the surface modified Polyimide
under low-pressure plasma will be characterized by contact
angle and surface energy measurement so as to identify best
wettability of the polymer surface. Physicochemical changes
of the Polymer surface under the exposure of low-pressure
plasma respectively will be characterized by various studies
under optical microscope, Scanning Electron Microscope and
X-ray Photoelectron Spectroscopy (XPS). Physicothermal
changes of Polyimide, Polyimide Adhesive and carbon nano
fiber dispersed Polyimide Adhesive will be characterized by
Differential Scanning Calorimetry (DSC) and Thermo
Gravimetric Analysis (TGA). Dispersion of carbon nano fiber
into the matrix Polyimide adhesive will be studied by Atomic
Force Microscopy (AFM). Lap shear tensile test under static
and dynamic load will be carried out to identify the best
adhesive joint. Durability studies of the best joint will be
carried out at different environmental conditions under
heating at different temperatures for specified time,
cryogenic temperature, exposing the joint to humid as well
as chemical climates and under intense high energy radiation
especially gamma radiation as well as neutron and proton
radiation related to GEO. Parallel experiments will monitor
changes in the properties of the polymer and adhesive itself
when subjected to these various environments. And finally,
under these environmental conditions, the durability of the
joints shall be correlated to the mode of failure of the
joints under static and dynamic loadings and failure
mechanism will also be correlated with stress distribution
of the joints using software of Finite Element Method.
Programme and Methodology
The aim of the proposed project is to produce
high performance nano adhesive bonds, suitable for use at
GEO between high temperature resistant polymers such as
Polyimide to Polyimide sheet (service temperature –250 0C to
+400 0C) by using ultra high temperature resistant Polyimide
adhesive, with the dispersion of Carbon Nano Fiber (CNF).
(i) Procurement of Materials
(a) Carbon Nano Fiber (CNF)
(b) Polyimide sheet
(c) Ultra High Temperature Resistant
Polyimide Adhesive
(ii) Studies on base Materials
(a) Surface characterization by
measuring contact angle and by estimating surface energy
(b) Surface characterization by XPS
and SIMS studies
(c) Optical microscope studies
(d) SEM (EDS) studies
(e) AFM studies
(f) DSC and TGA studies
(iii) Surface Modification
(a) Surface modification of Carbon
Nano Fiber (CNF) by low pressure plasma using nitrogen as
process gases
(b) Surface modification of polyimide
by low pressure plasma under various parameters and various
process gases
(iv) Surface Analysis after Modification
(a) Surface characterization by
measuring contact angle and by estimating surface energy
(b) Surface characterization by XPS
studies
(c) Optical microscope studies
(d) SEM (EDS) studies
(v) Dispersion of Carbon Nano Fiber (CNF) in Ultra High
Temperature Resistant Polyimide Adhesive
(a) AFM studies
(vi) Joining of Polyimide sheet with Polyimide sheet by the
above High Performance Nano Adhesive
(a) Polyimide sheet – Polyimide
Adhesive – Polyimide sheet
(b) Polyimide sheet –Nano Adhesive
(Polyimide Adhesive+CNF) – Polyimide sheet
(vii) Modification of the Polymer-Polymer Nano Adhesive
Bonding by Electron Beam Irradiation
(viii) Studies on Mechanical Properties of the Joints
(a) Lap shear tensile test under
static load
(b) Lap shear tensile test under
dynamic load
(ix) Fractographic Analysis of the Joints Fractures under
the Static and Dynamic Loadings
(a) XPS studies
(b) Optical microscope studies
(c) SEM (EDS) studies
(d) AFM studies
(x) Characterization of Joints Interfaces before and after
modification
(a) XPS studies
(b) Optical microscope studies
(c) SEM (EDS) studies
(d) AFM studies
(xi) Studies on Durability of the Best Joint obtained from
the mechanical test under various Environmental Conditions
(a) Heating at different temperatures
for specified time
(b) Cryogenic atmosphere
(c) Humidity and chemical atmosphere
(d) Ultraviolet and high energy
radiation
(e) Atomic oxygen atmosphere
(xii) Fractrographic Analysis of the Joints Fractured under
the Static and Dynamic Loadings after exposure to above
various Environmental Conditions
(a) XPS studies
(b) Optical microscope studies
(f) SEM (EDS) studies
(g) AFM studies
(xiii) Comparative Studies of Joint Strength and Fractograph
of the best joint before and after above various
Environmental Exposures
(xiv) Correlation of failure modes with stress distribution
along the interfaces by finite element software
(xv) Analysis of results
(xvi) Preparation of publications
Relevance to Beneficiaries
Adhesive bonding has many advantages over other ways of
joining materials, but its use is often restricted by
temperature and environmental limitations. This project will
ameliorate these limitations.
The advantages of adhesive bonds means that are widely used
throughout advanced manufacturing industry. For example they
are playing an increasingly important role in the
manufacture of vehicles for road, rail transport and
aerospace. In these areas the problems are analogous to
those in space applications, although far less acute. Thus
general manufacturing industry will certainly benefit from
the advances made in this project.
More, broadly, the project aims to elucidate the fundamental
mechanisms of adhesion in the bonds described and so will
also benefit all scientists working in the field of
adhesion.
Justification of Resources and Time
Schedule
Sikkim Manipal Institute of Technology (SMIT) under Sikkim
Manipal University (SMU), Sikkim, India has developed an
international collaboration with Adhesion Institute, Faculty
of Aerospace Engineering, Delft University of Technology,
The Netherlands with the appropriate facilities and ethos
that this implies. The two universities have also signed
Memorandum of Understanding (MOU) for Ph.D and Postdoctoral
Exchange Programme and SMIT (SMU) is going to establish a
centre of excellence ‘International Centre for Nano
Technology and Applied Adhesion’ (ICNTAA). ICNTAA of SMIT (SMU)
is also going to introduce M.Tech programme on Applied Nano
Technology (which is a combination Applied Adhesion and Nano
Technology). Moreover, SMIT (SMU) is the host institution
for 2nd Indo-SWISSBONDING International Congress in the
pattern of SWISSBONDING International Congress (www.swissbonding.ch)
to promoting knowledge on ‘Applied Adhesion and Nano
Technology’ in India. Much of the equipment needed for the
present investigation, is readily available due to the
collaboration with Faculty of Aerospace Engineering, Delft
University of Technology, The Netherlands. Therefore,
resources are only requested to purchasing materials, Salary
of one Senior Research Fellow (SRF) for three years, travel
expenses for attending and presenting research articles in
reputed International Conferences and collaborative visits
to Faculty of Aerospace Engineering, Delft University of
Technology, The Netherlands and purchasing one Atomic Force
Microscope (AFM) for ICNTAA. The AFM for ICNTAA will be
collective benefit for the institute, as SMIT (SMU) has
already undertaken three major Ph.D projects in this area,
and it will be very helpful for future M.Tech projects as
and when SMIT (SMU) has clear planning to start M.Tech
programme on Applied Nano Technology.
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References
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(1995), “Plasma Surface Modification of Propylene Based
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